View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 17192U 86097B 25349.94441718 .00000446 00000-0 48460-4 0 9991
2 17192 82.5059 221.0325 0015014 305.6527 65.2791 14.85805171 87910
| Epoch (UTC): | 15 December 2025 22:39:57 |
| Eccentricity: | 0.0015014 |
| inclination: | 82.5059° |
| perigee height: | 600 km |
| apogee height: | 621 km |
| right ascension of ascending node: | 221.0325° |
| argument of perigee: | 305.6527° |
| revolutions per day: | 14.85805171 |
| mean anomaly at epoch: | 65.2791° |
| orbit number at epoch: | 8791 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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